NORSAT 4, 62702
Orbit data source: Space-Track
NORSAT 4, 62702 is a payload satellite owned by NSC (NO) in SSO that was launched on Tue, 14 Jan 2025 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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62702 intel report (Beta)
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Identifier
Orbit
Country
NO / NORRelated business
Manufacturer
UTIAS-SFL
Mission
Operational Civil Com/Tech
Bus & Motor
DEFIANT, Unknown motor
Mass
35 kg wet, 35 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.6 m
Radar Cross Section
0.165 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 NORSAT 4
1 62702U 25009CX 26171.45821977 .00001072 00000-0 10312-3 0 9993
2 62702 97.7049 250.1067 0002620 57.6710 302.4764 14.95055233 77852Epoch: 2026-06-20T10:59Z
TLE epoch observation values (Epoch: 2026-06-20T10:59:50.188Z)
Latitude
-0.00001°
Longitude
176.47503°
Altitude
584.27 km
Speed
7.569 km/s
True Right ascension
16h 40m 25s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
07:19:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
581.036 km
Perigee altitude
577.391 km
Semi-major axis
6,957.35 km
Eccentricity
0.00026
Inclination
97.7049°
RAAN
250.1067°
Arg. of periapsis
57.671°
True anomaly
302.45107°
Mean anomaly
302.4764°
Eccentric anomaly
302.46373°
Mean motion
3.74005 °/min
Orbital period
96.26 mins
BSTAR
0.00010312
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Other satellites on launch #9 in the year 2025 (2025-01-14 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.NORSAT 4 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-06-21 04:47:47.714Z | 139° SSE | 2026-06-21 04:50:47.714Z | 86.021° E | 32.081° | 2026-06-21 04:54:47.714Z | 4.159° NNE |
| 6 mins | 2026-06-21 18:05:47.714Z | 16.004° NNE | 2026-06-21 18:08:47.714Z | 167.907° S | 43.277° | 2026-06-21 18:11:47.714Z | 189.737° SSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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